Title:
航空機のステアリング制御装置
Document Type and Number:
Japanese Patent JP6706677
Kind Code:
B2
Abstract:
A steering control apparatus for an aircraft is provided that can improve the travelling stability of an aircraft. An actual steering angle determining section (13) inside a steering control apparatus (1) determines an actual steering angle based on an actual steering amount. A target steering angle determining section (12) determines a target steering angle based on the operation amount of the steering gear. A target angle setting section (14) sets a target angle of a steered wheel. A control state switching section (11) switches between an enabled state in which steering control is performed to deflect the steered wheel such that the actual steering angle reaches the target angle and a disabled state in which the steering control is not performed. When the steering control state is switched to the enabled state, a correction section (141) inside the target angle setting section (14) sets an angle that was brought closer to the actual steering angle from the target steering angle, as the target angle. In addition, after the steering control state is switched to the enabled state, the correction section (141) brings the target angle closer to the target steering angle as time passes.
Inventors:
Yutaro Minami
Atsushi Yamazaki
Atsushi Yamazaki
Application Number:
JP2018539462A
Publication Date:
June 10, 2020
Filing Date:
September 15, 2016
Export Citation:
Assignee:
Sumitomo Precision Products Co., Ltd.
International Classes:
B64C25/50
Domestic Patent References:
| JP2013199201A | ||||
| JP2012218447A | ||||
| JP8133189A | ||||
| JP699893A | ||||
| JP2004255910A | ||||
| JP201286673A | ||||
| JP201318483A |
Foreign References:
| US5513821 | ||||
| US3885759 |
Attorney, Agent or Firm:
Ascend Patent Business Corporation